Computation spreading utilizing dithering for spur reduction in a digital phase lock loop

ABSTRACT

A novel and useful apparatus for and method of spur reduction using computation spreading with dithering in a digital phase locked loop (DPLL) architecture. A software based PLL incorporates a reconfigurable calculation unit (RCU) that is optimized and programmed to sequentially perform all the atomic operations of a PLL or any other desired task in a time sharing manner. An application specific instruction-set processor (ASIP) incorporating the RCU is adapted to spread the computation of the atomic operations out over a PLL reference clock period wherein each computation is performed at a much higher processor clock frequency than the PLL reference clock rate. This significantly reduces the per cycle current transient generated by the computations. The frequency content of the current transients is at the higher processor clock frequency which results in a significant reduction in spurs within sensitive portions of the output spectrum. Further reduction in spurs is achieved by dithering the duration of the software loop of atomic operations and/or by randomly shuffling one or more non-data dependent instructions within each iteration of the software loop.

REFERENCE TO RELATED APPLICATIONS

This application is related to U.S. Ser. No. 11/853,575, filed Sep. 11, 2007, entitled “Software reconfigurable digital phase lock loop architecture”, U.S. Ser. No. 11/853,588, filed Sep. 11, 2007, entitled “Computation spreading for spur reduction in a digital phase lock loop”, U.S. Ser. No. 11/949,310, filed Dec. 3, 2007, entitled “Computation parallelization in software reconfigurable all digital phase lock loop”, all of which are incorporated herein by reference in their entirety.

FIELD OF THE INVENTION

The present invention relates to the field of data communications and more particularly relates to an apparatus for and method of computation spreading using dithering to significantly reduce the generation of frequency spurs in a digital phase locked loop (DPLL) architecture.

BACKGROUND OF THE INVENTION

Phase locked loop (PLL) circuits are well known in the art. A block diagram illustrating an example prior art phase locked look (PLL) circuit is shown in FIG. 1. The typical PLL circuit, generally referenced 170, comprises phase detector 172, loop filter or low pass filter (LPF) 174 and voltage controlled oscillator (VCO) 176.

In operation, a frequency reference clock signal, often derived from a crystal oscillator, is input to the phase detector along with the VCO output signal (often divided down). The phase detector, typically implemented as a charge pump or mixer, generates a phase error (PHE) proportional to the phase difference between the reference clock input signal and the VCO output clock signal. The resultant PHE signal is then low pass filtered to yield a slow varying frequency command signal that controls the frequency of the VCO. The frequency command signal is input to a VCO or digitally controlled oscillator (DCO) such that the VCO output frequency/phase is locked to the reference clock with a certain fixed relationship. This oscillator generates an RF signal whose frequency depends on the frequency command signal.

In wireless communication systems, e.g., GSM, UMTS, Bluetooth, WiFi, etc., the RF synthesizer is a fundamental block that is used to provide a high quality, high frequency RF carrier for the transmitter and a local oscillator clock for the receiver, whose output frequency can range from several hundreds of MHz to several GHz. Different applications with different standards require different RF frequencies with different RF performance requirements. The RF clock generating the RF carrier plays a critical role in the entire wireless communication system. The quality of the RF clock directly affects the communication performance and often is the determining factor whether the system meets standards specifications.

Typically, the RF synthesizer is implemented using a phase locked loop (PLL) typically using a pure hardwired (i.e. largely fixed hardware with limited reconfigurability) design approach. All digital phase locked loops (ADPLLs) for RF synthesizer construction targeting wireless communications are known in the art. Conventional ADPLL circuits, however, are implemented as fixed hardware based (or hardwired) with limited reconfigurability. It is thus difficult for one design to readily support multi-standard wireless applications, e.g., GSM, GPRS, EDGE, WCDMA, etc. as well as wireless data networks, such as Bluetooth, WiFi and WiMAX.

Once a hardwired circuit design is committed to a physical implementation, there is little that can be changed regarding the transfer function or operation of the ADPLL. Any modification requiring logic and interconnect change results in numerous time consuming steps within the ASIC creation process (i.e. timing closure, physical design, etc.) typically requiring significant engineering resources and months of delay to launch a product. In addition, once the silicon is manufactured, any change to the ADPLL architecture makes an even costlier impact, making such changes virtually impractical.

In general, a main difference between a hardwired implementation and a microprocessor based implementation is that the microprocessor implementation uses shared hardware running at higher speed, while the hardwired implementation uses dedicated hardware running at lower speed. A block diagram illustrating an example prior art generalized processing block using a dedicated hardware implementation is shown in FIG. 2. The hardwired implementation, generally referenced 10, comprises a plurality of dedicated hardware blocks 12 for each function 14. The circuit provides memory (Mem1, Mem2, Mem3, Mem4) and dedicated hardware for each function (F1, F2, F3, F4), wherein each block runs at the data path speed f_(s).

A block diagram illustrating an example prior art generalized processing block using a processor based implementation is shown in FIG. 3. The circuit, generally referenced 16, comprises instruction memory 18, instruction fetch 20, instruction decode 22, ALU 24, data bus 29, register file 26 and data memory 28. The processor based solution has one shared hardware block ALU that can be configured to execute any of the four functions (F1, F2, F3, F4). The ALU is programmed by the instructions stored in instruction memory 18 and the ALU is adapted to run four times faster (4f_(s)) to complete the data processing within the data path speed of f_(s).

With CMOS process technology currently advancing from 65 nm to 45 nm to 32 nm, transistors are becoming faster and faster. The interconnections, however, are becoming more and more dominant in SOC design regarding the delay and area contribution. The interconnections in a hardwired design having a large area will significantly slow the circuit speed while adding a significant silicon area overhead. Since processor based solutions run at higher speed with shared hardware, resulting in smaller area, advancements in semiconductor technology will make processor based solutions more and more attractive. This further favors use of multiple but smaller processors with a dedicated instruction set rather than one processor with a more general instruction set.

Furthermore, in conventional ADPLL circuits, the digital part of local oscillator (DLO) (i.e. a portion of the ADPLL) is implemented using dedicated random logic gates. Thus, all computations are launched on the rising edge of the ADPLL system reference clock and latched on the next rising edge. Since a majority of the circuit switching activity is centered on the rising edge of the system reference clock, most of the digital current is being switched at that point as well, creating large current transients. These digital current surges find their way into on-chip DCO, LNA, mixer and PA circuit nodes via various coupling mechanisms, e.g., capacitive, etc. These disturbances at the system clock rate have strong harmonics that are upconverted into sensitive areas of the RF spectrum, resulting in unacceptable RF spurious tones.

It is thus desirable to have a processor based PLL architecture that is software based and programmable. The programmable PLL should provide a reconfiguration capability which eases silicon debugging and development tasks and provides multi-standard operation capability. Further, the software based PLL architecture should create significantly lower current transients thus reducing the generation of spurs in the output spectrum. At the same time, the unavoidable spurious energy that is generated by the logic activity and coupled into RF circuits should be pushed higher in frequency where they lie outside of or can be easily filtered out of critical frequency bands.

SUMMARY OF THE INVENTION

The present invention is a novel and useful apparatus for and method of spur reduction using computation spreading and dithering in a digital phase locked loop (DPLL) architecture. The invention is particularly suitable for use with a software based phase locked loop (PLL). The processor-based PLL (i.e. all digital phase-locked loop or ADPLL) architecture described herein can be used for RF frequency synthesis in radio transceivers and other applications.

The software based phase locked loop incorporates a reconfigurable calculation unit (RCU) that can be programmed to sequentially perform all the atomic operations of a phase locked loop or any other desired task. The RCU is a key component in a so called application specific instruction-set processor (ASIP). The ASIP includes an instruction set that comprises instructions optimized to perform the individual atomic operations of a phase locked loop.

The reconfigurable computational unit (RCU) is time shared for all computations within the phase locked loop. The reconfigurable computational unit and related configuration control logic replaces the dedicated and distributed random logic inside the conventional digital PLL. The reconfigurable computational unit is controlled via microcode stored in on-chip memory (e.g., RAM or ROM). Since the computational unit is time shared among all operations, it is operated at an oversampled rate that is high enough to insure the proper implementation of the phase locked loop. In order to achieve this, the reconfigurable computational unit is optimized to perform all computations of the phase locked loop atomic operations within a single reference clock cycle.

In one embodiment, the instruction set is implemented in microcode that is stored in volatile or non-volatile memory. Thus, the ASIP can easily be reconfigured to implement customized designs for different applications, such as multiple cellular standards, including GSM, GPRS, EDGE, WCDMA, Bluetooth, WiFi, etc., as well as wireless data network standards, including Bluetooth, WiFi, WiMAX, etc. The ASIP can be configured on the fly to handle the different RF frequency and performance requirements of each communication standard. The software based PLL of the present invention provides the flexibility for a more unified design that fits different applications.

In another embodiment, the phase locked loop task is partitioned into a plurality of atomic operations. The ASIP is adapted to spread the computation of the atomic operations out over and completed within an entire PLL reference clock period. Each computation being performed at a much higher processor clock frequency than the PLL reference clock rate. This functions to significantly reduce the per cycle current transient generated by the computations. Further, the frequency content of the current transients is at the higher processor clock frequency. This results in a significant reduction in spurs within sensitive portions of the output spectrum.

In addition, dithering is introduced to further reduce frequency spurs in the band of interest. In one embodiment, the duration of the software loop is dithered around the nominal clock period by adding a single wait cycle to the software loop. In another embodiment, the spurs are further reduced by spreading a plurality of wait cycles throughout the software loop. In yet another embodiment, the spurs are reduced by shuffling (randomly or pseudo-randomly) one or more non-data dependent instructions in each iteration of the software loop.

An example application is provided of the software based phase locked loop incorporated in a single chip radio, e.g., Bluetooth, GSM, etc., that integrates the RF circuitry with the digital base band (DBB) circuitry on the same die.

Advantages of the software reconfigurable phase locked loop of the present invention include the following. Firstly, the invention enables all phase domain calculations to be performed within one reference clock cycle due to the use of the reconfigurable calculation unit optimized for performing PLL calculations serially at high frequency. Secondly, defining the ASIP instruction set in microcode stored in volatile or non-volatile memory makes it inherently software reconfigurable, permitting the microcode to be replaced without changing any lithography masks. The enables easier silicon debugging and multi-standard radio support.

Thirdly, the invention permits a significant reduction in silicon area. The invention trades the rate of operation for the amount of active implementation area required by the process of oversampling and function sharing. For an X factor increase in operational frequency, there is a complimentary X factor decrease in the required computational combinatorial logic area. An additional area is needed due to the overhead of computational unit multiplexing. While the storage area is constant, the net result is a significant reduction in overall implementation area required.

Fourthly, the invention enables a significant reduction of RF spurs in the sensitive frequency bands of a radio by changing the frequency of the switching logic gates. Prior art solutions perform PLL computations at relatively low rates, e.g., FREF of 26-38.8 MHz. The resulting switching current transients are mixed with the carrier and appear as frequency spurs at sensitive radio frequency bands. Considering GSM, for example, the most sensitive RX band is approximately 20 to 80 MHz away from the carrier. The invention performs the bulk of computations at oversampled rates, resulting in spurs outside sensitive regions. The amount of oversampling can be controlled (e.g., increased or decreased) to provide any desired frequency planning by changing the frequency of the processing clock. Fifthly, reduction in silicon area provided by the invention enables power routing and decoupling capacitance requirements to be relaxed.

Note that some aspects of the invention described herein may be constructed as software objects that are executed in embedded devices as firmware, software objects that are executed as part of a software application on either an embedded or non-embedded computer system such as a digital signal processor (DSP), microcomputer, minicomputer, microprocessor, etc. running a real-time operating system such as WinCE, Symbian, OSE, Embedded LINUX, etc. or non-real time operating system such as Windows, UNIX, LINUX, etc., or as soft core realized HDL circuits embodied in an Application. Specific Integrated Circuit (ASIC) or Field Programmable Gate Array (FPGA), or as functionally equivalent discrete hardware components.

There is this provided in accordance with the invention, a method of reducing the generation of frequency spurs in the performance of a processing task normally performed within a reference clock period, the method comprising the steps of dividing the task into a plurality of atomic operation computations for execution in a software loop, randomizing the execution of one or more atomic operations in each iteration of the software loop and wherein the atomic operations are clocked using a processor clock having a frequency significantly higher than that of the reference clock.

There is also provided in accordance with the invention, a method of reducing the generation of frequency spurs in a software based digital phase locked loop normally performed within a reference clock period, the method comprising the steps of dividing computation of the phase locked loop operation into a plurality of atomic operation computations for execution in a software loop, dithering the duration of each iteration of the software loop and wherein the atomic operations are clocked using a processor clock having a frequency significantly higher than that of the reference clock.

There is further provided in accordance with the invention, a method of reducing the generation of frequency spurs in a software based digital phase locked loop normally performed within a reference clock period, the method comprising the steps of dividing computation of the phase locked loop operation into a plurality of atomic operation computations for execution in a software loop, dithering the duration of each iteration of the software loop by inserting a plurality of random wait periods throughout the software loop and wherein the atomic operations are clocked using a processor clock having a frequency significantly higher than that of the reference clock.

There is also provided in accordance with the invention, a method of reducing the generation of frequency spurs in a software based digital phase locked loop normally performed within a reference clock period, the method comprising the steps of dividing computation of the phase locked loop operation into a plurality of atomic operation computations for execution in a software loop, randomly shuffling the order of execution of one or more atomic operations in each iteration of the software loop and wherein the atomic operations are clocked using a processor clock having a frequency significantly higher than that of the reference clock.

There is further provided in accordance with the invention, a phase locked loop (PLL) having a reference clock, the PLL comprising means for partitioning computation of the phase locked loop into a plurality of atomic operation computations for execution in a software loop, means for randomizing the execution of one or more atomic operations in each iteration of the software loop, a processor clock having a frequency significantly higher than that of the reference clock, an oscillator operative to generate a radio frequency (RF) signal having a frequency determined in accordance with a tuning command input thereto and a processor operative to generate the tuning command, the processor clocked at the processor clock rate, the processor comprising a calculation unit operative to execute instructions, wherein each instruction is operative to perform one of the atomic operation computations.

BRIEF DESCRIPTION OF THE DRAWINGS

The invention is herein described, by way of example only, with reference to the accompanying drawings, wherein:

FIG. 1 is a block diagram illustrating a simplified block diagram of an example prior art phase locked look (PLL) circuit;

FIG. 2 is a block diagram illustrating an example prior art generalized processing block using a dedicated hardware implementation;

FIG. 3 is a block diagram illustrating an example prior art generalized processing block using a processor based implementation;

FIG. 4 is a block diagram illustrating a single chip polar transmitter based radio incorporating a software based DPLL using dithering mechanism of the present invention;

FIG. 5 is a simplified block diagram illustrating an example mobile communication device incorporating the software based DPLL using dithering mechanism of the present invention;

FIG. 6 is a block diagram illustrating functions of an example ADPLL-based polar transmitter suitable for use with the present invention;

FIG. 7 is a simplified block diagram illustrating an embodiment of the software based ADPLL incorporating a processor based phase domain calculator;

FIG. 8 is a block diagram illustrating an example embodiment of the phase domain calculator of the present invention in more detail;

FIG. 9 is a timing diagram illustrating the processing clock and reference frequency timing;

FIG. 10 is a block diagram illustrating an instruction view of the software based ADPLL architecture of the present invention;

FIG. 11 is a block diagram illustrating an example processor based software ADPLL architecture of the present invention;

FIG. 12A is a diagram illustrating the output and transfer function equations for the infinite impulse response (IIR) filter portion of the ADPLL;

FIG. 12B is an equivalent block diagram implementing the output equation shown in FIG. 12A;

FIG. 12C is an equivalent block diagram implementing the output equation shown in FIG. 12A whereby the multiplication operations have been replaced with shift operations;

FIG. 12D is a diagram illustrating the resultant reconfigurable calculation unit (RCU) implementing the output equation shown in FIG. 12A;

FIG. 13 is a block diagram illustrating an example RCU unit for implementing the ADPLL circuit;

FIG. 14 is a block diagram illustrating the RCU unit for implementing the F_Diff( ) instruction;

FIG. 15 is a block diagram illustrating the RCU unit for implementing the F_PheAcc( ) instruction;

FIG. 16 is a block diagram illustrating the RCU unit for implementing the F_IIR( ) instruction;

FIG. 17 is a block diagram illustrating the RCU unit for implementing the F_SHR( ) instruction;

FIG. 18 is a block diagram illustrating the RCU unit for implementing the F_IntAcc( ) instruction;

FIG. 19 is a block diagram illustrating the RCU unit for implementing the F_SHRAdd( ) instruction;

FIG. 20 is a timing diagram illustrating several ADPLL processing clock options and the current spikes resulting therefrom;

FIG. 21 is a timing diagram illustrating an example RF spectrum generated by a legacy ADPLL;

FIG. 22 is a timing diagram illustrating an example RF spectrum generated by the software based ADPLL of the present invention;

FIG. 23 is a flow diagram illustrating the RF spur reduction method of the present invention;

FIG. 24 is a diagram illustrating a spurious frequency pattern with 3.8 MHz gaps between spurs;

FIG. 25 is a diagram illustrating a spurious frequency pattern with 2.0 MHz gaps between spurs;

FIG. 26 is a diagram illustrating a spurious frequency pattern with 0.7 MHz gaps between spurs;

FIG. 27 is a diagram illustrating the relationship between loop size and spur gap;

FIG. 28 is a diagram illustrating a square wave with and without dithering;

FIG. 29 is a diagram illustrating the power spectral density of the square wave without dithering;

FIG. 30 is a diagram illustrating the power spectral density of the square wave with dithering;

FIG. 31 is an example listing of a variable duration software loop with a single wait cycle;

FIG. 32 is a flow diagram illustrating a first software dithering method of the present invention;

FIG. 33 is a diagram illustrating the instruction current waveform for a software loop having eight instructions and eight wait cycles;

FIG. 34 is a diagram illustrating the power spectral density for fixed size software loops;

FIG. 35 is a diagram illustrating the instruction current waveform for a software loop with varying wait time;

FIG. 36 is a diagram illustrating the power spectral density for a software loop having a variable size;

FIG. 37 is an example listing of a variable duration software loop with multiple wait cycles;

FIG. 38 is a flow diagram illustrating a second software dithering method of the present invention;

FIG. 39 is a diagram illustrating the instruction current waveform for a variable duration software loop with multiple wait cycles;

FIG. 40 is a diagram illustrating the power spectral density for a software loop with multiple wait cycles;

FIG. 41 is an example listing of a software loop with one or more shuffled instructions;

FIG. 42 is a flow diagram illustrating a second software dithering method of the present invention;

FIG. 43 is a diagram illustrating the current waveform with a different power level for each instruction;

FIG. 44 is a diagram illustrating the power spectral density for a software loop with different instruction power;

FIG. 45 is a diagram illustrating the instruction current waveform for a software loop with one or more shuffled instructions;

FIG. 46 is a diagram illustrating the power spectral density for a software loop with one or more shuffled instructions; and

FIG. 47 is a block diagram illustrating hardware dithering through clock gating.

DETAILED DESCRIPTION OF THE INVENTION Notation Used Throughout

The following notation is used throughout this document.

Term Definition AC Alternating Current ACL Asynchronous Connectionless Link ACW Amplitude Control Word ADC Analog to Digital Converter ADPLL All Digital Phase Locked Loop ALU Arithmetic Logic Unit AM Amplitude Modulation ASIC Application Specific Integrated Circuit ASIP Application Specific Instruction-set Processor AVI Audio Video Interface AWS Advanced Wireless Services BIST Built-In Self Test BMP Windows Bitmap BPF Band Pass Filter CMOS Complementary Metal Oxide Semiconductor CPU Central Processing Unit CU Control Unit CW Continuous Wave DAC Digital to Analog Converter dB Decibel DBB Digital Baseband DC Direct Current DCO Digitally Controlled Oscillator DCXO Digitally Controlled Crystal Oscillator DPA Digitally Controlled Power Amplifier DPLL Digital Phase Locked Loop DRAC Digital to RF Amplitude Conversion DRP Digital RF Processor or Digital Radio Processor DSL Digital Subscriber Line DSP Digital Signal Processor EDGE Enhanced Data Rates for GSM Evolution EDR Enhanced Data Rate EEPROM Electrically Erasable Programmable Read Only Memory EPROM Erasable Programmable Read Only Memory eSCO Extended Synchronous Connection-Oriented FCC Federal Communications Commission FCW Frequency Command Word FIB Focused Ion Beam FM Frequency Modulation FPGA Field Programmable Gate Array FSM Finite State Machine GMSK Gaussian Minimum Shift Keying GPRS General Packet Radio Service GPS Global Positioning System GSM Global System for Mobile communications HB High Band HDL Hardware Description Language HFP Hands Free Protocol I/F Interface IC Integrated Circuit IEEE Institute of Electrical and Electronics Engineers IIR Infinite Impulse Response JPG Joint Photographic Experts Group LAN Local Area Network LB Low Band LDO Low Drop Out LNA Low Noise Amplifier LO Local Oscillator LPF Low Pass Filter MAC Media Access Control MAP Media Access Protocol MBOA Multiband OFDM Alliance MIM Metal Insulator Metal Mod Modulo MOS Metal Oxide Semiconductor MP3 MPEG-1 Audio Layer 3 MPG Moving Picture Experts Group MUX Multiplexer NZIF Near Zero IF OFDM Orthogonal Frequency Division Multiplexing PA Power Amplifier PAN Personal Area Network PC Personal Computer PCI Personal Computer Interconnect PD Phase Detector PDA Personal Digital Assistant PE Phase Error PHE Phase Error PLL Phase Locked Loop PM Phase Modulation PPA Pre-Power Amplifier QoS Quality of Service RAM Random Access Memory RCU Reconfigurable Calculation Unit RF Radio Frequency RFBIST RF Built-In Self Test RMS Root Mean Squared ROM Read Only Memory SAM Sigma-Delta Amplitude Modulation SAW Surface Acoustic Wave SCO Synchronous Connection-Oriented SEM Spectral Emission Mask SIM Subscriber Identity Module SoC System on Chip SRAM Static Read Only Memory SYNTH Synthesizer TDC Time to Digital Converter TDD Time Division Duplex TV Television UART Universal Asynchronous Transmitter/Receiver UGS Unsolicited Grant Services UMTS Universal Mobile Telecommunications System USB Universal Serial Bus UWB Ultra Wideband VCO Voltage Controlled Oscillator WCDMA Wideband Code Division Multiple Access WiFi Wireless Fidelity WiMAX Worldwide Interoperability for Microwave Access WiMedia Radio platform for UWB WLAN Wireless Local Area Network WMA Windows Media Audio WMAN Wireless Metropolitan Area Network WMV Windows Media Video WPAN Wireless Personal Area Network XOR Exclusive Or ZIF Zero IF

Detailed Description of the Invention

The present invention is a novel and useful apparatus for and method of RF spur reduction using computation spreading and dithering in a digital phase locked loop (DPLL) architecture. The invention is particularly suitable for use with a software based phase locked loop (PLL). The processor-based PLL (i.e. all digital phase-locked loop or ADPLL) architecture described herein can be used for RF frequency synthesis in radio transceivers and other applications.

A software based PLL incorporates a reconfigurable calculation unit (RCU) that is optimized and programmed to sequentially perform all the atomic operations of a PLL or any other desired task in a time sharing manner. An application specific instruction-set processor (ASIP) incorporating the RCU is adapted to spread the computation of the atomic operations out over and completed within an entire PLL reference clock period. Each computation being performed at a much higher processor clock frequency than the PLL reference clock rate. This functions to significantly reduce the per cycle current transient generated by the computations. Further, the frequency content of the current transients is at the higher processor clock frequency. This results in a significant reduction in spurs within sensitive portions of the output spectrum.

An example application is provided of the software based phase locked loop incorporated in a single chip radio, e.g., Bluetooth, GSM, etc., that integrates the RF circuitry with the digital baseband (DBB) circuitry on the same die.

Although the RF spur reduction with dithering mechanism is applicable to numerous wireless communication standards and can be incorporated in numerous types of wireless or wired communication devices such a multimedia player, mobile station, cellular phone, PDA, DSL modem, WPAN device, etc., it is described in the context of a Digital RF Processor (DRP™) based transceiver that may be adapted to comply with a particular wireless communications standard such as GSM, Bluetooth, EDGE, WCDMA, WLAN, WiMax, etc. It is appreciated, however, that the invention is not limited to use with any particular communication standard and may be used in optical, wired and wireless applications. Further, the invention is not limited to use with a specific modulation scheme but is applicable to numerous modulation schemes.

Note that throughout this document, the term communications device is defined as any apparatus or mechanism adapted to transmit, receive or transmit and receive data through a medium. The term communications transceiver is defined as any apparatus or mechanism adapted to transmit and receive data through a medium. The communications device or communications transceiver may be adapted to communicate over any suitable medium, including wireless or wired media. Examples of wireless media include RF, infrared, optical, microwave, UWB, Bluetooth, WiMAX, WiMedia, WiFi, or any other broadband medium, etc. Examples of wired media include twisted pair, coaxial, optical fiber, any wired interface (e.g., USB, Firewire, Ethernet, etc.). The term Ethernet network is defined as a network compatible with any of the IEEE 802.3 Ethernet standards, including but not limited to 10Base-T, 100Base-T or 1000Base-T over shielded or unshielded twisted pair wiring. The terms communications channel, link and cable are used interchangeably. The notation DRP is intended to denote either a Digital RF Processor or Digital Radio Processor. References to a Digital RF Processor infer a reference to a Digital Radio Processor and vice versa.

The term multimedia player or device is defined as any apparatus having a display screen and user input means that is capable of playing audio (e.g., MP3, WMA, etc.), video (AVI, MPG, WMV, etc.) and/or pictures (JPG, BMP, etc.). The user input means is typically formed of one or more manually operated switches, buttons, wheels or other user input means. Examples of multimedia devices include pocket sized personal digital assistants (PDAs), personal media player/recorders, cellular telephones, handheld devices, and the like.

Some portions of the detailed descriptions which follow are presented in terms of procedures, logic blocks, processing, steps, and other symbolic representations of operations on data bits within a computer memory. These descriptions and representations are the means used by those skilled in the data processing arts to most effectively convey the substance of their work to others skilled in the art. A procedure, logic block, process, etc., is generally conceived to be a self-consistent sequence of steps or instructions leading to a desired result. The steps require physical manipulations of physical quantities. Usually, though not necessarily, these quantities take the form of electrical or magnetic signals capable of being stored, transferred, combined, compared and otherwise manipulated in a computer system. It has proven convenient at times, principally for reasons of common usage, to refer to these signals as bits, bytes, words, values, elements, symbols, characters, terms, numbers, or the like.

It should be born in mind that all of the above and similar terms are to be associated with the appropriate physical quantities they represent and are merely convenient labels applied to these quantities. Unless specifically stated otherwise as apparent from the following discussions, it is appreciated that throughout the present invention, discussions utilizing terms such as ‘processing,’ ‘computing,’ ‘calculating,’ ‘determining,’ ‘displaying’ or the like, refer to the action and processes of a computer system, or similar electronic computing device, that manipulates and transforms data represented as physical (electronic) quantities within the computer system's registers and memories into other data similarly represented as physical quantities within the computer system memories or registers or other such information storage, transmission or display devices.

The invention can take the form of an entirely hardware embodiment, an entirely general-purpose software embodiment or an embodiment containing a combination of hardware and software elements. In one embodiment, a portion of the mechanism of the invention is implemented in software, which includes but is not limited to firmware, resident software, object code, assembly code, microcode, etc.

Furthermore, the invention can take the form of a computer program product accessible from a computer-usable or computer-readable medium providing program code for use by or in connection with a computer or any instruction execution system. For the purposes of this description, a computer-usable or computer readable medium is any apparatus that can contain, store, communicate, propagate, or transport the program for use by or in connection with the instruction execution system, apparatus, or device, e.g., floppy disks, removable hard drives, computer files comprising source code or object code, flash semiconductor memory (USB flash drives, etc.), ROM, EPROM, or other semiconductor memory devices.

Single Chip Radio

A block diagram illustrating a single chip radio incorporating a software based ADPLL mechanism of the present invention is shown in FIG. 4. For illustration purposes only, the transmitter, as shown, is adapted for the GSM/EDGE/WCDMA cellular standards. It is appreciated, however, that one skilled in the communication arts can adapt the transmitter and receiver illustrated herein to other modulations and communication standards as well without departing from the spirit and scope of the present invention.

The radio, generally referenced 30, comprises a radio integrated circuit 31 coupled to a crystal 38, RF front end module 46 coupled to an antenna 44, and battery management circuit 32 coupled to battery 68. The radio chip 31 comprises a script processor 60, digital baseband (DBB) processor 61, memory 62 (e.g., static RAM), TX block 42, RX block 58, digitally controlled crystal oscillator (DCXO) 50, slicer 51, power management unit 34 and RF built-in self test (BIST) 36. The TX block comprises high speed and low speed digital logic block 40 including ΣΔ modulators (not shown), phase domain calculator using dithering (ASIP) 52, digitally controlled oscillator (DCO) 56, accumulator 59, sampler 69 and digitally controlled power amplifier (DPA) 48. The RX block comprises a low noise transconductance amplifier 63, current sampler 64, discrete time processing block 65, analog to digital converter (ADC) 66 and digital logic block 67.

The principles presented herein have been used to develop three generations of a Digital RF Processor (DRP): single-chip Bluetooth, GSM and GSM/EDGE radios realized in 130 nm, 90 nm and 65 nm digital CMOS process technologies, respectively. This architecture is also used as the foundation for a UMTS single-chip radio manufactured using a 45 nm CMOS process. The common architecture is highlighted with features added specific to the cellular radio. The all digital phase locked loop (ADPLL) based transmitter employs a polar architecture with all digital phase/frequency and amplitude modulation paths. The receiver employs a discrete-time architecture in which the RF signal is directly sampled and processed using analog and digital signal processing techniques.

A key component is the digitally controlled oscillator (DCO) 56, which avoids any analog tuning controls. A digitally-controlled crystal oscillator (DCXO) generates a high-quality base station-synchronized frequency reference such that the transmitted carrier frequencies and the received symbol rates are accurate to within 0.1 ppm. Fine frequency resolution for both DCO and DCXO is achieved through high-speed ΣΔ dithering of their varactors. Digital logic built around the DCO realizes an all-digital PLL (ADPLL) that is used as a local oscillator for both the transmitter and receiver. The polar transmitter architecture utilizes the wideband direct frequency modulation capability of the ADPLL and a digitally controlled power amplifier (DPA) 48 for the amplitude modulation. The DPA operates in near-class-E mode and uses an array of nMOS transistor switches to regulate the RF amplitude. It is followed by a matching network and an external front-end module 46, which comprises a power amplifier (PA), a transmit/receive switch for the common antenna 44 and RX surface acoustic wave (SAW) filters. Fine amplitude resolution is achieved through high-speed ΣΔ dithering of the DPA nMOS transistors.

The receiver 58 employs a discrete-time architecture in which the RF signal is directly sampled at the Nyquist rate of the RF carrier and processed using analog and digital signal processing techniques. The transceiver is integrated with a script processor 60, dedicated digital base band processor 61 (i.e. ARM family processor and/or DSP) and SRAM memory 62. The script processor handles various TX and RX calibration, compensation, sequencing and lower-rate data path tasks and encapsulates the transceiver complexity in order to present a much simpler software programming model.

The frequency reference (FREF) is generated on-chip by a 26 MHz (or any other desired frequency, such as 13 or 38.4 MHz) digitally controlled crystal oscillator (DCXO) 50, which provides negative resistance to sustain the oscillations. The output of the DCXO is coupled to slicer 51. The output of the slicer is input to the phase domain calculator which comprises a software based PLL in accordance with the invention and described in more detail infra.

An integrated power management (PM) system 34 is connected to an external battery management circuit 32 that conditions and stabilizes the supply voltage. The PM comprises multiple low drop out (LDO) regulators that provide internal supply voltages and also isolate supply noise between circuits, especially protecting the DCO. The RF built-in self-test (RFBIST) 36 performs autonomous phase noise and modulation distortion testing, various loopback configurations for bit-error rate measurements and implements the DPA calibration and BIST mechanism. The transceiver is integrated with the digital baseband, SRAM memory in a complete system-on-chip (SoC) solution. Almost all the clocks on this SoC are derived from and are synchronous to the RF oscillator clock. This helps to reduce susceptibility to the noise generated through clocking of the massive digital logic.

The transmitter comprises a polar architecture in which the amplitude and phase/frequency modulations are implemented in separate paths. Transmitted symbols generated in the digital baseband (DBB) processor are first pulse-shape filtered in the Cartesian coordinate system. The filtered in-phase (I) and quadrature (Q) samples are then converted through a CORDIC algorithm into amplitude and phase samples of the polar coordinate system. The phase is then differentiated to obtain frequency deviation. The polar signals are subsequently conditioned through signal processing to sufficiently increase the sampling rate in order to reduce the quantization noise density and lessen the effects of the modulating spectrum replicas.

A more detailed description of the operation of the ADPLL can be found in U.S. Patent Publication No. 2006/0033582 A1, published Feb. 16, 2006, to Staszewski et al., entitled “Gain Calibration of a Digital Controlled Oscillator,” U.S. Patent Publication No. 2006/0038710 A1, published Feb. 23, 2006, Staszewski et al., entitled “Hybrid Polar/Cartesian Digital Modulator” and U.S. Pat. No. 6,809,598, to Staszewski et al., entitled “Hybrid Of Predictive And Closed-Loop Phase-Domain Digital PLL Architecture,” all of which are incorporated herein by reference in their entirety.

Mobile Device/Cellular Phone/PDA System

A simplified block diagram illustrating an example mobile communication device incorporating the software based DPLL with dithering mechanism of the present invention is shown in FIG. 5. The communication device may comprise any suitable wired or wireless device such as a multimedia player, mobile station, mobile device, cellular phone, PDA, wireless personal area network (WPAN) device, Bluetooth EDR device, etc. For illustration purposes only, the communication device is shown as a cellular phone or smart phone. Note that this example is not intended to limit the scope of the invention as the software based DPLL using dithering mechanism of the present invention can be implemented in a wide variety of wireless and wired communication devices.

The mobile station, generally referenced 70, comprises a baseband processor or CPU 71 having analog and digital portions. The MS may comprise a plurality of RF transceivers 94 and associated antenna(s) 98. RF transceivers for the basic cellular link and any number of other wireless standards and RATs may be included. Examples include, but are not limited to, Global System for Mobile Communication (GSM)/GPRS/EDGE 3G; CDMA; WiMAX for providing WiMAX wireless connectivity when within the range of a WiMAX wireless network using OFDMA techniques; Bluetooth for providing Bluetooth wireless connectivity when within the range of a Bluetooth wireless network; WLAN for providing wireless connectivity when in a hot spot or within the range of an ad hoc, infrastructure or mesh based wireless LAN network; near field communications; 60G device; UWB; etc. One or more of the RF transceivers may comprise an additional a plurality of antennas to provide antenna diversity which yields improved radio performance. The mobile station may also comprise internal RAM and ROM memory 111, Flash memory 112 and external memory 114. Note that the mechanism of the invention is operative to not only reduce spurious content or emissions of a wireless standard pertaining to a particular radio but to also reduce interference between different radios operating simultaneously, which enhances coexistence.

Several user interface devices include microphone(s) 84, speaker(s) 82 and associated audio codec 80 or other multimedia codecs 75, a keypad for entering dialing digits 86, vibrator 88 for alerting a user, camera and related circuitry 101, a TV tuner 102 and associated antenna 104, display(s) 106 and associated display controller 108 and GPS receiver 90 and associated antenna 92. A USB or other interface connection 78 (e.g., SPI, SDIO, PCI, etc.) provides a serial link to a user's PC or other device. An FM receiver 72 and antenna 74 provide the user the ability to listen to FM broadcasts. SIM card 116 provides the interface to a user's SIM card for storing user data such as address book entries, etc. Note that the SIM card shown is intended to represent any type of smart card used for holding user related information such as identity and contact information, Authentication Authorization and Accounting (AAA), profile information, etc. Different standards use different names, for example, SIM for GSM, USIM for UMTS and ISIM for IMS and LTE.

The mobile station comprises software based DPLL using dithering blocks 125 which may be implemented in any number of the RF transceivers 94. Alternatively, or in addition to, the software based DPLL using dithering block 128 may be implemented as a task executed by the baseband processor 71. The software based DPLL using dithering blocks 125, 128 are adapted to implement the software based DPLL using dithering mechanism of the present invention as described in more detail infra. In operation, the software based DPLL using dithering blocks may be implemented as hardware, software or as a combination of hardware and software. Implemented as a software task, the program code operative to implement the software based DPLL using dithering mechanism of the present invention is stored in one or more memories 111, 112 or 114 or local memories within the baseband processor.

Portable power is provided by the battery 124 coupled to power management circuitry 122. External power is provided via USB power 118 or an AC/DC adapter 120 connected to the battery management circuitry which is operative to manage the charging and discharging of the battery 124.

Example ADPLL Polar Transmitter

A block diagram illustrating an example ADPLL-based polar transmitter for wireless applications is shown in FIG. 6. The example ADPLL shown is used as the basis for a software based DPLL using dithering mechanism described in more detail infra. A more detailed description of the operation of the ADPLL can be found in U.S. Patent Publication No. 2006/0033582 A1, published Feb. 16, 2006, to Staszewski et al., entitled “Gain Calibration of a Digital Controlled Oscillator,” U.S. Patent Publication No. 2006/0038710 A1, published Feb. 23, 2006, Staszewski et al., entitled “Hybrid Polar/Cartesian Digital Modulator” and U.S. Pat. No. 6,809,598, to Staszewski et al., entitled “Hybrid Of Predictive And Closed-Loop Phase-Domain Digital PLL Architecture,” all of which are incorporated herein by reference in their entirety.

For illustration purposes only, the transmitter, as shown, is adapted for the GSM/EDGE/WCDMA cellular standards. It is appreciated, however, that one skilled in the communication arts can adapt the transmitter illustrated herein to other modulations and communication standards as well without departing from the spirit and scope of the present invention.

The transmitter, generally referenced 130, is well-suited for a deep-submicron CMOS implementation. The transmitter comprises a complex pulse shaping filter 168, amplitude modulation (AM) block 169 and ADPLL 132. The circuit 130 is operative to perform complex modulation in the polar domain in addition to the generation of the local oscillator (LO) signal for the receiver. All clocks in the system are derived directly from this source. Note that the transmitter is constructed using digital techniques that exploit the high speed and high density of the advanced CMOS, while avoiding problems related to voltage headroom. The ADPLL circuit replaces a conventional RF synthesizer architecture (based on a voltage-controlled oscillator (VCO) and a phase/frequency detector and charge-pump combination), with a digitally controlled oscillator (DCO) 148 and a time-to-digital converter (TDC) 162. All inputs and outputs are digital and some even at multi-GHz frequency.

The core of the ADPLL is a digitally controlled oscillator (DCO) 148 adapted to generate the RF oscillator clock CKV. The oscillator core (not shown) operates at a multiple of the 1.6-2.0 GHz (e.g., 4) high band frequency or at a multiple of the 0.8-1.0 GHz low band frequency (e.g., 8). Note that typically, the multiple is a power-of-two but any other suitable integer or even fractional frequency relationship may be advantageous. The output of the DCO is then divided for precise generation of RX quadrature signals, and for use as the transmitter's carrier frequency. The single DCO is shared between transmitter and receiver and is used for both the high frequency bands (HB) and the low frequency bands (LB). In addition to the integer control of the DCO, at least 3-bits of the minimal varactor size used are dedicated for ΣΔ dithering in order to improve frequency resolution. The DCO comprises a plurality of varactor banks, which may be realized as n-poly/n-well inversion type MOS capacitor (MOSCAP) devices or Metal Insulator Metal (MIM) devices that operate in the flat regions of their C-V curves to assist digital control. The output of the DCO is a modulated digital signal at f_(RF). This signal is input to the pre-power amplifier (PPA) 152. It is also input to the RF low band pre-power amplifier 154 after divide by two via divider 150.

The expected variable frequency f_(V) is related to the reference frequency f_(R) by the frequency command word (FCW).

$\begin{matrix} {{F\; C\; {W\lbrack k\rbrack}} \equiv \frac{E\left( {f_{V}\lbrack k\rbrack} \right)}{f_{R}}} & (1) \end{matrix}$

The FCW is time variant and is allowed to change with every cycle T_(R)=1/f_(R) of the frequency reference clock. With W_(F)=24 the word length of the fractional part of FCW, the ADPLL provides fine frequency control with 1.5 Hz accuracy, according to:

$\begin{matrix} {{\Delta \; f_{res}} = \frac{f_{R}}{2^{W_{F}}}} & (2) \end{matrix}$

The number of integer bits W_(I)=8 has been chosen to fully cover the GSM/EDGE and partial WCDMA band frequency range of f_(V)=1,600-2,000 MHz with an arbitrary reference frequency f_(R)≧8 MHz.

The ADPLL operates in a digitally-synchronous fixed-point phase domain as follows: The variable phase accumulator 156 determines the variable phase R_(V)[i] by counting the number of rising clock transitions of the DCO oscillator clock CKV as expressed below.

$\begin{matrix} {{R_{V}\lbrack i\rbrack} = {\sum\limits_{l = 0}^{i}1}} & (3) \end{matrix}$

The index i indicates the DCO edge activity. The variable phase R_(V)[i] is sampled via sampler 158 to yield sampled FREF variable phase R_(V)[k], where k is the index of the FREF edge activity. The sampled FREF variable phase R_(V)[k] is fixed-point concatenated with the normalized time-to-digital converter (TDC) 162 output ε[k]. The TDC measures and quantizes the time differences between the frequency reference FREF and the DCO clock edges. The sampled differentiated (via block 160) variable phase is subtracted from the frequency command word (FCW) by the digital frequency detector 138. The frequency error f_(E)[k] samples

f _(E) [k]=FCW−[(R _(V) [k]−ε[k])−(R _(V) [k−1]−ε[k−1])]  (4)

are accumulated via the frequency error accumulator 140 to create the phase error φ_(E)[k] samples

$\begin{matrix} {{\varphi_{E}\lbrack k\rbrack} = {\sum\limits_{l = 0}^{k}{f_{E}\lbrack k\rbrack}}} & (5) \end{matrix}$

which are then filtered by a fourth order IIR loop filter 142 and scaled by a proportional loop attenuator α. A parallel feed with coefficient ρ adds an integrated term to create type-II loop characteristics which suppress the DCO flicker noise.

The IIR filter is a cascade of four single stage filters, each satisfying the following equation:

y[k]=(1−λ)·y[k−1]+λ·x[k]  (6)

wherein

x[k] is the current input;

y[k] is the current output;

k is the time index;

X is the configurable coefficient;

The 4-pole IIR loop filter attenuates the reference and TDC quantization noise with an 80 dB/dec slope, primarily to meet the GSM/EDGE spectral mask requirements at 400 kHz offset. The filtered and scaled phase error samples are then multiplied by the DCO gain K_(DCO) normalization factor f_(R)/{circumflex over (K)}_(DCO) via multiplier 146, where f_(R) is the reference frequency and {circumflex over (K)}_(DCO) is the DCO gain estimate, to make the loop characteristics and modulation independent from K_(DCO). The modulating data is injected into two points of the ADPLL for direct frequency modulation, via adders 136 and 144. A hitless gear-shifting mechanism for the dynamic loop bandwidth control serves to reduce the settling time. It changes the loop attenuator α several times during the frequency locking while adding the (α₁/α₂−1)φ₁ dc offset to the phase error, where indices 1 and 2 denote before and after the event, respectively. Note that φ₁=φ₂, since the phase is to be continuous.

The frequency reference FREF is input to the retimer 166 and provides the clock for the TDC 162. The FREF input is resampled by the RF oscillator clock CKV via retimer block 166 which may comprise a flip flop or register clocked by the reference frequency FREF. The resulting retimed clock (CKR) is distributed and used throughout the system. This ensures that the massive digital logic is clocked after the quiet interval of the phase error detection by the TDC. Note that in the example embodiment described herein, the ADPLL is a discrete-time sampled system implemented with all digital components connected with all digital signals.

Software Based ADPLL Architecture

A simplified block diagram illustrating an embodiment of the software based ADPLL incorporating a processor based phase domain calculator is shown in FIG. 7. The ADPLL circuit, generally referenced 180, comprises a phase domain calculator 174, DCO 186, integer feedback block 188, fractional feedback block 189 and programmable fractional-N clock divider 182.

In operation, the phase domain calculator replaces the conventional ADPLL circuit with a software based ADPLL. As with the conventional ADPLL, it is operative to generate the DLO update that is input to the DCO 186 which in turn generates the RF output frequency clock CKV. The phase domain calculator receives the FCW commands, variable phase information (i.e. integer and fractional feedback) and the reference frequency clock FREF, which typically ranges between 13 and 52 MHz. The processing clock output of the programmable clock divider 182 runs at a frequency significantly higher than FREF, such as in the range 200 to 600 MHz, for example.

In accordance with the invention, the phase domain calculator performs the ADPLL operations serially rather than in parallel. In order the complete the ADPLL computation within reference clock cycle, the much faster processor clock is used to clock the phase domain calculator internal circuitry.

The solution uses a reconfigurable computational unit (RCU) or ALU (described infra) that is time shared for most or all computations within the ADPLL. The RCU and its related configuration control logic (constituting a special purpose microcomputer) replaces the dedicated and distributed random logic within a conventional ADPLL. The RCU is controlled via microcode stored in on-chip memory such as random access memory (RAM), read only memory (ROM), Flash memory, etc. Since the computational unit is time shared among most operations, it is operated at a much higher clock rate than the conventional ADPLL which performs all calculations in parallel using dedicated hardware circuits. The RCU circuitry is optimized to perform all the required ADPLL atomic computations within one reference clock cycle.

A block diagram illustrating an example embodiment of the phase domain calculator of the present invention in more detail is shown in FIG. 8. The phase domain calculator, generally referenced 190, comprises an ALU (or RCU) 202, instruction and data memory 192, register file 194, sequencer 196, latches 208, 206, multiplexers 209, 198, 200, 204.

The instructions for implementing the ADPLL operation are stored in the instruction memory. Instructions are input to the sequencer which performs the instruction decoding and generates the appropriate signals to execute each instruction. The register file stores intermediate values calculated by the ALU.

A timing diagram illustrating the processing clock and reference frequency timing is shown in FIG. 9. As shown, the processing clock 210, used to clock the memory, sequencer and register file, is at a significantly higher clock rate than the reference clock FREF 212. This is required in order the complete an operation cycle of the ADPLL within a single reference clock period.

A block diagram illustrating an instruction view of the software based ADPLL architecture of the present invention is shown in FIG. 10. The circuit, generally referenced 220, comprises a phase calculation unit 222, gain normalization 238, DCO 240, gain calibration 242, accumulator/incrementer 244 and variable phase sampler 246. The phase calculation unit shows an instruction view of the ADPLL architecture performed in software. In particular, the phase calculation unit 222 comprises a phase detector 224, frequency error accumulator 226, IIR loop filter 228, a proportional gain multiplier 230, IIR filter 232, adder 234, DCO gain multiplier 236, offset phase error adder 248, phase error accumulator 250 and integral or p gain multiplier 252. Both proportional and integral multipliers preferably use power-of-two arithmetic so that their respective multipliers could be implemented as bit-shift operators. For non-power-of-two arithmetic, sum-of-power-of-two or even full multipliers can be used with the consequent increase in circuit cost and complexity.

The ADPLL circuit shown is an ADPLL architecture that is commonly used in wireless applications for RF frequency generation. In this digital architecture, the traditional VCO is replaced with a digitally controlled oscillator (DCO) and the oscillating frequency of the DCO is controlled by a frequency command word (FCW) instead of the reference clock, as described in detail supra. The phase detecting and filtering parts are all digital with intensive digital signal processing involved as highlighted.

In operation, the ADPLL operation is partitioned into a plurality of atomic operations, wherein each atomic operation performs a complete processing step within the ADPLL. For example, an adding operation representing adder 224 comprises one atomic operation. Similarly, accumulation block 226 and each of four elemental first-order IIR operations in IIR filter block 228 also comprise a single atomic operation each. Each atomic operation is performed by a separate instruction. Individual instructions are provided for each atomic operation in the ADPLL (or any other task).

The computation elements within the phase calculation block 222 are the elements implemented and executed as software instructions. The computations within block 222 can be expressed as pseudo code as shown in the following Listing 1.

Listing 1: Sequential pseudo-code for ADPLL phase computation L1: y16 = y15 − S1 // S1 is the store element S1 = y15 // delay y1 = FCW − y16 y2 = y2 + y1 // accumulation y3 = IIR (a1, y2, y3) // 4th order infinite impulse response(IIR) filter y4 = IIR (a2, y3, y4) y5 = IIR (a3, y4, y5) y6 = IIR (a4, y5, y6) y7 = SHL (y6, alpha) // shift operation y11 = IIR (gs, y7, y11) y9 = y6 − PhE y10 = y10 + y9 // implies accumulation y12 = SHL (y10, rho) y13 = y11 + y12 y14 = y13 * gain jump L1 // operates in a continuous loop

As described supra, in prior art ADPLL circuits, all ADPLL phase computations are implemented using dedicated hardware (i.e. a hardwired design), which limits the ability to adjust the ADPLL algorithm. In accordance with the software based architecture of the present invention, these ADPLL functions are integrated within a processor using shared hardware thereby providing significant flexibility to the ADPLL algorithm.

Processor Based ADPLL Architecture

A block diagram illustrating an example processor based software ADPLL architecture of the present invention is shown in FIG. 11. The ADPLL circuit, generally referenced 260, comprises an application specific instruction-set processor (ASIP) 262, DCO 286, accumulator 288 and variable phase sampler 289. The ASIP 262 comprises instruction memory 264, fetch block 266, decode block 268, data bus 278, RCU 270, S-unit 272, L-unit 274, A-unit 276, register file 280, data memory 282 and interface 284.

All ADPLL computations as delineated in Listing 1 above are incorporated into a so-called Application Specific Instruction-set Processor (ASIP) 262. It is appreciated that a general purpose processor may also be used to perform the ADPLL operation. An ASIP, however, is far more efficient due to the instruction set being adapted to perform a small but dedicated set of atomic operations.

In operation, the ASIP processor stores the ADPLL software instructions in the instruction memory 264. The instructions are then fetched from the instruction memory via fetch block 266 and fed into the decoding block 268. All required control signals are generated through the decoding block to control the operation of the various computational units, including the A-Unit 276 for performing arithmetic operations, e.g., addition, subtraction, etc., L-Unit 274 for performing logic operations, e.g., AND, OR, XOR, etc. and S-Unit 272 for performing data storage and movement operations. A reconfigurable calculation unit (RCU) 270 is constructed to provide application specific instructions for the ADPLL. The RCU, for example, is operative to implement the 1-stage IIR filtering operation within a single instruction. It is noted that the application driven customized instruction set is what differentiates an ASIP from a general purpose processor which performs ADPLL computations much less efficiently to the extent that it may not even be able to complete the necessary computations within the reference clock period.

The ASIP processor is operative to read the FCW and variable phase (PhV) inputs, sequentially perform all the computations (i.e. atomic operations) required for the ADPLL as presented in Listing 1 within one system reference clock cycle and send the resulting tuning word DCO_TUNE (i.e. DLO update) to the DCO. which in turn uses the tuning word to adjust its output frequency. It is important to note that all the computations are performed via the programmed software stored in instruction memory of the ASIP. Note also that the majority of the computations are performed by the RCU, which is designed specifically to implement the atomic operations of the targeted ADPLL application.

Reconfigurable Calculation Unit (RCU)

The structure of the RCU will now be described in more detail. As described above, all the computations in Listing 1 are described in terms of atomic arithmetic operations, such as additions, subtractions, shifting, multiplications, etc. and as more complicated operations, such as IIR filtering. A prior art hardwired implementation simply instantiates the number of hardware operators equal to the number of atomic operations required by the ADPLL algorithm. This, however, has its drawbacks as discussed supra.

The ASIP based design of the present invention utilizes one or more reconfigurable computational units that are used to perform all arithmetic operations implementing the ADPLL algorithm. This computational unit is “recycled” sequentially among all the arithmetic operations within a single cycle of the ADPLL system clock. The internal state of the ADPLL is stored between clock cycles in internal storage elements (i.e. register file, data memory, etc.). An important aspect of the RCU design is the greatly increased application efficiency along with a maximization of resource reuse.

Detailed knowledge of the task to be implemented (e.g., ADPLL algorithm) is important in creating the functionality of the computational unit in order to optimize its complexity and system throughput requirements. In the case of an ADPLL algorithm, all the elemental ADPLL computations (except for IIR filtering) are either add/subtract or power-of-two multiply operation. Therefore, the invention provides for a single IIR computation that has been optimized to be represented as a single operation in the computational unit.

FIGS. 12A, 12B, 12C and 12D illustrate the mapping process and the resulting configuration of the RCU. In particular, FIG. 12A is a diagram illustrating the output and transfer function equations for the infinite impulse response (IIR) filter portion of the ADPLL. FIG. 12B is an equivalent block diagram implementing the output equation shown in FIG. 12A. The circuit, generally referenced 290, comprises multipliers 292, 298, adders 294, 299 and unit delay 296.

FIG. 12C is an equivalent block diagram implementing the output equation shown in FIG. 12A whereby the multiplication operations have been replaced with shift operations. The circuit, generally referenced 300, comprises shift operations 302, 309, adders 304, 308 and unit delay 306. FIG. 12D is a diagram illustrating the resultant reconfigurable calculation unit (RCU) implementing the output equation shown in FIG. 12A. The RCU, generally referenced 310, comprises shifter 312, 318 and adders 314, 316. The unit delay element is replaced with data lines Rb and Rd for reading and writing to an external memory such as the register file or data memory.

Thus, for application to an ADPLL, the multiplication operation in the IIR filter is simplified with a shifting operation. The final RCU in 12D is a pure computation unit without any storage element. To map the IIR equation below

y _(k)=(1−a)·y _(k−1) +a·x _(k)   (7)

to the RCU unit, the following applies:

x_(k) maps to RCU input Ra;

y_(k−1) maps to RCU input Rb;

y_(k) maps to RCU output Rd;

The RCU unit is made further configurable to accommodate all the main computations for the ADPLL in an efficient manner. A block diagram illustrating an example RCU unit for implementing the ADPLL circuit way is shown in FIG. 13. The RCU and related circuitry, generally referenced 320, comprises a plurality of elements as follows: two data inputs (Ra, Rb), two data outputs (Rd_st, Rd), three atomic computation units (first addition/subtraction 324, shifter 326, second addition/subtraction 328), two latch/storage elements (input latch S_d 336 and output latch Rd 330), local registers for data storage, e.g., shift amount a, FCW 340, PhE 342, multiplexers for data steering 332, 334 and control/configure signals.

In operation, the RCU takes input data Ra and goes through the first addition/subtraction followed by a shifting operation followed by a second addition/subtraction. The data is then sent to the outside register file Rd_st or latched (Rd) for the next computation. An input latching element (S_d) is included as part of a differentiation operation. All the computation units including the data paths inside the RCU are configurable with the control/configure signals generated by the ASIP decoding block.

Table 1 below shows the mapping of the customized instruction set provided by the RCU and their corresponding targeted computations in the ADPLL.

TABLE 1 Customized instructions and their corresponding computations in the ADPLL Computations in ADPLL Customized Instructions L1: y16 = y15 − S_d F_Diff (y15, y16) S_d = y15 y1 = FCW − y16 F_PheAcc (y1, y2) y2 = y2 + y1 y3 = IIR (a1, y2, y3) F_IIR1 (y2, y3) y4 = IIR (a2, y3, y4) F_IIR2 (y3, y4) y5 = IIR (a3, y4, y5) F_IIR3 (y4, y5) y6 = IIR (a4, y5, y6) F_IIR4 (y5, y6) y7 = SHR (y6, alpha) F_SHR (y6, y7) y11 = IIR(gs, y7, y11) F_IIRgs (y7, y11) y9 = y6 − PhE F_IntAcc (y6, y10) y10 = y10 + y9 y12 = SHR (y10, rho) F_SHRAdd (y10, y11, y13) y13 = y11 + y12 y14 = y13 * gain F_Gain( ) jump L1 NA

Detailed descriptions for most of the instructions in Table 1 above are provided below. For each instruction, a corresponding figure is provided illustrating the data paths and computation elements in the RCU used in executing the instruction. Elements in each of the figures described below operate as described above in connection with FIG. 13. Further, the bold lines or arrows in each figure highlight the data path for that particular instruction.

F_Diff Instruction

F_Diff(y15, y16): y16=y15−S _(—) d

S _(—) d=y15

A block diagram illustrating the RCU unit 350 for implementing the F_Diff( ) instruction is shown in FIG. 14. The F_Diff instruction implements a differentiation operation. The bold arrow lines highlight the data path in the RCU. Input y15 is received and the first addition/subtraction unit is bypassed (e.g., the second or negating input to the first adder is set to zero). The shifting unit is also bypassed and a subtraction (via the second addition/subtraction unit) is performed with local register S_d. The result y16 is output via Rd_st. The instruction also updates S_d with input y15 via register latch S_d.

F_PheAcc Instruction

F_PheAcc(y16, y2): y1=FCW−y16

y2=y2+y1;

A block diagram illustrating the RCU unit 352 for implementing the F_PheAcc( ) instruction is shown in FIG. 15. This instruction implements a subtraction plus an accumulation operation. It takes the input y16, performs the accumulation operation using the first addition/subtraction unit, bypasses any shifting (i.e. the shifter is configured for pass through operation). A subtraction operation with local register FCW is then performed. The accumulation is done on the Rd register latch.

F_IIR Instruction

F_IIR( ): Rd=Rb>>(1−a)+Ra>>a

A block diagram illustrating the RCU unit 354 for implementing the F_IIR( ) instruction is shown in FIG. 16. This instruction implements an IIR filtering operation. The shift amount ‘a’ is pre-set locally within the RCU. Thus, the RCU is optimized to have the capability of performing an IIR filter operation in a single instruction cycle. This permits an efficient computation of the atomic operations needed to implement the ADPLL within a single reference clock period.

F_SHR Instruction

F_SHR(Ra, Rd): Rd=Ra>>a

A block diagram illustrating the RCU unit 356 for implementing the F_SHR( ) instruction is shown in FIG. 17. This instruction implements a shifting operation. The shift amount ‘a’ is pre-set locally within the RCU. The two addition/subtraction units are bypassed for this instruction.

F_IntAcc Instruction

F_IntAcc(y6, y10): y9=y6−PhE

y10=y10+y9

A block diagram illustrating the RCU unit 358 for implementing the F_IntAcc( ) instruction is shown in FIG. 18. This instruction implements a subtraction and an accumulation operation. It takes the input y16, performs an accumulation in the first addition/subtraction unit and then bypasses the shifter. A subtraction is then performed using local register PhE.

F_SHRAdd Instruction

F_SHRAdd(y10, y11, y13): y12=SHR(y10, rho)

y13=y11+y12

A block diagram illustrating the RCU unit 360 for implementing the F_SHRAdd( ) instruction is shown in FIG. 19. This instruction implements a shifting operation followed by an addition operation. The shift amount RHO is set locally in the RCU. Input y10 is received, the first addition/subtraction unit is bypassed and then a shifting operation is performed. The shifter output then undergoes an addition operation via the second addition/subtraction unit.

F_Gain Instruction

The F_Gain( ) instruction performs a multiplication by a gain value. In the case where the gain value is a power of two, the shift operation is used to perform this instruction. For non power of two gain values, a multiplier in the RCU is used (not shown).

In addition to the instructions described in detail hereinabove, the RCU comprises other customized instructions that are needed for general purpose applications, such as for setting RCU local register values, etc.

RF Spur Reduction

The effects of the software based ADPLL on RF spur reduction will now be described. As described supra, in prior art single-chip radios, the phase domain calculation portion of the ADPLL signal processing is traditionally implemented using dedicated random logic gates. In such an implementation, all computations are initiated on a rising edge of the ADPLL system clock and latched on the subsequent rising edge of the clock. This is shown in FIG. 20 which illustrates a timing diagram of several ADPLL processing clock options and the current spikes resulting therefrom. Trace 370 is the FREF system reference clock while trace 374 represents the processor clock.

Since the majority of circuit switching activity in the PLL (and also other close-in circuitry) is centered on a rising edge of the FREF system clock, most of the digital current is being switched at this edge as well, as indicated by trace 372. It is noted that depending on the particular implementation of the flip-flop registers, the current induced by the falling edge of the clock could be substantial. These digital current surges find their way into on-chip DCO and PA circuit nodes in the transmitter and LNA and mixer nodes in the receiver via various parasitic coupling mechanisms. The current rush energy due to digital processing at the system clock rate gets upconverted into the RF spectrum by the DCO, resulting in unacceptable RF spurs that are close in frequency to the carrier or fall into the protected frequency bands, such as the receive band, GPS band, etc. The Federal Communications Commission (FCC) rules and numerous wireless communication standards place very low limits on the energy outside of the information carrying frequency range that is allowed to be radiated from wireless terminals. In the receiver, the spurious tones in the local oscillator (LO) can degrade blocking or interferer performance through reciprocal mixing.

These low frequency RF spurs are normally very difficult to filter out in a wireless terminal before they are radiated by the antenna because of their proximity in the spectrum to the carrier as shown in FIG. 21. The FREF clock spurs 384 are shown around the carrier 382. The filtering envelope 380 will not sufficiently attenuate the spurs to meet the various wireless standards. This is because a high order filtering is required to block the undesired energy, i.e. a steep filter envelope is required. The typical combined filtering effects of the PA (power amplifier), SAW filter and antenna filter out only a portion of the energy of these undesired RF spurs, thus making FCC rules and wireless standard compliance extremely difficult to meet.

In contrast, the mechanism of the present invention is operative to perform the atomic operations serially at the much faster processor rate. At each processor cycle, only a single instruction is executed resulting in reduced current transients being generated, as indicated in trace 376. This results in significantly reduced RF spur generation. In the present invention, the effects these generated spurs have on RF performance are two-fold: (1) the spurs are shifted to higher frequencies where they are easier to filter out by the oscillator's LC tank, DPA matching network, PA matching network, bandpass filtering in the RF front-end module, as well as overall parasitic RC (resistor-capacitor) network; and (2) the energy of each spur is reduced.

In accordance with the invention, the software based ADPLL significantly reduces the generation of RF spurs in sensitive frequency bands of the DRP by changing the frequency plan of the switching logic gates. The ASIP/RCU performs the bulk of computations at the processor clock rate which is much higher in frequency than that of the system reference clock (FREF). This results in the RF spurs being shifted outside the sensitive regions close to the carrier frequency as shown in FIG. 22. The processing clock spurs 392 are now far away from the carrier 392 and the filtering envelope 390 is able to remove these spurs with ease.

It is noted that the total amount of energy consumed in performing computations in the conventional ADPLL and the software based ADPLL of the invention is substantially the same. The frequency content of this energy, however, is significantly different. In case of the conventional ADPLL, the computation energy is concentrated at the reference clock edges and therefore has strong low frequency harmonic.

In case of the software based ADPLL, the computation energy is spread out between the reference clock edges (which may or may not coincide with the processor clock edges). The spreading out of the computation energy over the reference clock period serves to create a much higher frequency harmonic. When these harmonics mix with the carrier, they are offset in frequency around the carrier. The filtering requirements to remove the undesired RF spurs close to the carrier are excessive, as in the case of the conventional ADPLL. The further away from the carrier the RF spurs are located, the more relaxed the filtering requirements become. Changing the frequency content of the computation energy to (1) improve the RF spectrum characteristics or (2) consider one or more protected frequency bands (e.g., RX band, GPS band) is referred to as frequency planning. Such frequency planning also helps to relax circuit design constraints, such as power routing resistance and decoupling capacitance values, which contribute to the magnitude of the energy surges at the clock edges.

Further, the frequency planning can be modified by varying the amount of oversampling (i.e. the ratio of processor clock frequency to the reference frequency FREF). The frequency planning can be lowered as long as the minimum required processing throughput in the processor is maintained. Otherwise, the required atomic operations of the ADPLL may not be completed within a reference clock cycle.

It is appreciated that the application of the software based mechanism described herein is not limited to an ADPLL. The mechanism can be applied to any computing or processing task that can benefit from reduced spur generation. A flow diagram illustrating the RF spur reduction method of the present invention is shown in FIG. 23. In the general case, the task is first partitioned into a plurality of atomic operations (step 400). The computation of the atomic operations required to complete the task are spread out and/or reshuffled over an entire reference clock period (step 402). The computation of each atomic operation occurs at the higher processor clock rate, rather that the slower reference clock rate (step 404).

Software Dithering to Reduce Frequency Spurs

As described infra, the software ADPLL is operative to push the frequency spurs from a low reference clock frequency to a high processor clock frequency. The software running in the processor, however, contains the low frequency software loops, which still function to create low frequency energy spikes. To illustrate this, an example is shown below. The example software loop demonstrates how the loop size of the script processor (i.e. the control processor within radio, e.g., block 60 in FIG. 4) affects the spur pattern generated. Assume the script processor runs the following simple loop shown in Listing 2 below:

Listing 2: Example software loop L1: R4 = [5, 10, 30] // [Fig. 24, Fig. 25, Fig. 26], respectively while (R4 != 0) {   R4 = R4 − 1 } jump L1 // operates in a continuous loop

A diagram illustrating a spurious frequency pattern with 3.8 MHz gaps between spurs is shown in FIG. 24. In this graph, the channel frequency is set to 1859 MHz and R4=5. The graph shows a spurious pattern having frequency gaps of approximately 3.8 MHz between spurs.

A diagram illustrating a spurious frequency pattern with 2.0 MHz gaps between spurs is shown in FIG. 25. In this graph, the channel frequency is set to 1859 MHz and R4=10. The graph shows a spurious pattern having frequency gaps of approximately 2.0 MHz between spurs.

A diagram illustrating a spurious frequency pattern with 0.7 MHz gaps between spurs is shown in FIG. 26. In this graph, the channel frequency is set to 1859 MHz and R4=30. The graph shows a spurious pattern having frequency gaps of approximately 0.7 MHz between spurs.

For a value of R4=15, the gap between frequency spurs is approximately 1.4 MHz. It is noted that the frequency gap between these related spurs is proportional to the loop frequency (i.e. loop size), as shown in FIG. 27 wherein trace 410 represents the data calculated in accordance with the expression y=23/(x+1) and trace 423 represents measured data. As the loop size increases, i.e. loop frequency decreases, the spur gaps decreases.

Thus, continuing to change the loop size causes the energy of the loop frequency spurs to be spread out. The following example is presented to illustrate this. A diagram illustrating a square wave with and without dithering is shown in FIG. 28 wherein trace 414 represents a square wave without dithering and trace 416 represents a square wave with dithering. The first waveform 414 is a uniform square wave having a period of 1 μs. The second waveform 416 is a square wave having a varied period. The period of waveform 416 changes and repeats in accordance with the following pattern: 10/8 μs, 1 μs, 10/8 μs, 6/8 μs, 9/8 μs, 5/8 μs, 7/8 μs, 10/8 μs, 7/8 μs, 9/8 μs, 1 μs, 6/8 μs, 10/8 μs, 5/10 μs, 10/8 μs, 7/8 μs, 9/8 μs, etc. It is important to note that the average period of waveform 416 with dithering is still 1 μs, the same as waveform 414 without dithering.

A diagram illustrating the power spectral density of the square wave 414 (FIG. 28) without dithering is shown in FIG. 29. Note that the spectrum contains spikes at the main frequency (i.e. 1 MHz) and its harmonics. A diagram illustrating the power spectral density of the square wave 416 (FIG. 28) with dithering is shown in FIG. 30. It is important to note that by simply dithering the period of the square wave, the peak spurs power is reduced by more than 6 dB. The power at those peak frequencies is spread out to other frequencies since the total power must remain the same.

In accordance with the invention, the technique of changing the loop size is applied to the data sample based operation such as the software based DPLL. In the software based DPLL, considering a reference clock of 26 MHz (i.e. data samples arrive at the processor at a rate of 26 MHz), then the software loop also runs at 26 MHz. In general, however, the processor will likely have some level of MIPS margin. In this case, the processor finishes processing the current data sample and waits for the next data sample to arrive. In particular, it waits at the end of the software loop for the next data sample to arrive. Preferably, a mechanism to maintain the correct average processing rate is used. Such a mechanism could be implicitly realized or one or more extra steps are included in the method.

Using the pseudo-code in Listing 1 presented supra as an example, a wait instruction is inserted at the end of the loop, as shown below in Listing 3.

Listing 3: Pseudo-code for ADPLL phase computation with wait instruction L1: y16 = y15 − S1 // S1 is the store element S1 = y15 // delay y1 = FCW − y16 y2 = y2 + y1 // accumulation y3 = IIR (a1, y2, y3) // 4th order infinite impulse response(IIR) filter y4 = IIR (a2, y3, y4) y5 = IIR (a3, y4, y5) y6 = IIR (a4, y5, y6) y7 = SHL (y6, alpha) // shift operation y11 = IIR (gs, y7, y11) y9 = y6 − PhE y10 = y10 + y9 // implies accumulation y12 = SHL (y10, rho) y13 = y11 + y12 y14 = y13 * gain wait_data // wait for next data sample to arrive jump L1 // operates in a continuous loop

If the system comprises a relatively small sized buffer (i.e. FIFO) for the data samples, then the wait time can be adjusted such that the software loop waits a different number of cycles for different data samples.

Listing 4: Pseudo-code for ADPLL phase computation with randomized wait time L1: y16 = y15 − S1 // S1 is the store element S1 = y15 // delay y1 = FCW − y16 y2 = y2 + y1 // accumulation y3 = IIR (a1, y2, y3) // 4th order infinite impulse response(IIR) filter y4 = IIR (a2, y3, y4) y5 = IIR (a3, y4, y5) y6 = IIR (a4, y5, y6) y7 = SHL (y6, alpha) // shift operation y11 = IIR (gs, y7, y11) y9 = y6 − PhE y10 = y10 + y9 // implies accumulation y12 = SHL (y10, rho) y13 = y11 + y12 y14 = y13 * gain wait r0 // wait for r0 cycles, r0 changes each iteration of // the loop in accordance with a predetermined // pattern of randomized values jump L1 // operates in a continuous loop

In the pseudo-code in Listing 4, register r0 is set to a random value at each iteration of the software loop. The values for r0 may be set in accordance with a predetermined random value pattern. Each instruction in the software loop will have a similar repeating pattern as that of waveform 416 (FIG. 28). Thus, the coupling energy of each instruction will have the similar spreading effects as analyzed for the waveforms in FIG. 28.

A flow diagram illustrating a first software dithering method of the present invention is shown in FIG. 32. First, the task (e.g., DPLL computation) is partitioned into a plurality of atomic operations (step 420). A randomized wait instruction is inserted in the loop, typically, but not necessarily, at the end of the software loop (step 422). The atomic operations of the software loop are executed over a reference clock cycle (step 424). The wait instruction causes the loop to pause a randomized number of cycles (step 426). The wait period each iteration may be set in accordance with a predetermined wait pattern.

A generalized version of Listing 4 is shown in FIG. 31 wherein the duration of the software loop varies from iteration to iteration in accordance with the predetermined pattern of random numbers r0 is set to.

To simplify the analysis, consider the following example pseudo-code shown below in Listing 5:

Listing 5: Example software loop L1: Instruction1 Instruction2 Instruction3 Instruction4 Instruction5 Instruction6 Instruction7 Instruction8 wait 8 cycles jump L1 // operates in a continuous loop

We further assume that each instruction generates the same current on the power supply. A diagram illustrating the instruction current waveform for a software loop having eight instructions and eight wait cycles is shown in FIG. 33. A diagram illustrating the power spectral density for fixed size software loops (i.e. without dithering) is shown in FIG. 34. The main spikes occur at the instruction clock frequency (i.e. 200 MHz) and its harmonics. All the other spurs occur at the loop frequency (i.e. 12.5 MHz) and its harmonics.

In accordance with the present invention, the waiting time for each loop is randomized (i.e. dithered). A diagram illustrating the instruction current waveform for a software loop with randomized wait time is shown in FIG. 35. Note the randomized wait times between the clusters of instructions. A diagram illustrating the corresponding power spectral density for a software loop having a variable duration (i.e. length) is shown in FIG. 36. The randomization of the wait times cases a significant change in the corresponding power spectral density. It is noted that the loop frequency spurs are reduced due to the loop size varying from one iteration of the software loop to the next.

In another embodiment, a plurality of waiting cycles are further spread out within the software loop and blended in with the instructions. Both the location of and the time duration of each wait cycle can be randomized. An example listing of a variable duration software loop with multiple wait cycles is shown in FIG. 37. This generalized listing shows four wait cycles, i.e. wait r0, wait r1, wait r2 and wait r3, spread throughout the software loop. The values of r0, r1, r2 and r3 may be set in accordance with a predetermined pattern of random wait times. As in the previous embodiment comprising a single wait cycle (e.g., at the end of the software loop), the total wait time of the plurality of wait cycles should not exceed what it would have been with a single wait cycle. Thus, the dithering of the length of the software loop is now divided over a plurality of wait cycles instead of just one. Wherein each wait cycle is programmed with a random pattern of wait times such that the overall affect of dithering the length of the software loop is still achieved.

A flow diagram illustrating a second software dithering method of the present invention is shown in FIG. 38. First, the task (e.g., DPLL computation) is partitioned into a plurality of atomic operations (step 430). A plurality of randomized wait instructions are placed throughout the software loop (step 432). Preferably, they are placed asymmetrically throughout the loop. Random wait patterns are generated for each of the wait instructions (step 434). The atomic operations of the software loop are executed over a reference clock cycle (step 436). The execution of each wait instruction causes the loop to pause a randomized number of cycles (step 438). The wait period at each wait cycle over each iteration may be set in accordance with a predetermined wait pattern.

A diagram illustrating the instruction current waveform for a variable duration software loop with multiple wait cycles is shown in FIG. 39. Compared to the graph of FIG. 35, the instruction current waveform in FIG. 39 are further spread out and randomized in time. A diagram illustrating the power spectral density for a software loop with multiple wait cycles is shown in FIG. 40. In this graph, corresponding to the instruction current waveform of FIG. 39, the frequency spurs have become cleaner with regard to the main (i.e. major or large) spikes of FIG. 36.

In yet another embodiment, one or more instructions within the software loop are shuffled in random fashion. The shuffling may be performed randomly or pseudo-randomly. Randomly shuffling the instructions changes the repeating cycles of each instruction, which has the similar effect as changing the loop size for those instructions. Note that only instructions that are not data dependent are shuffled. Instructions that depend on certain data must be executed in their proper order, otherwise the DPLL computation (or other task computation) will not be carried out properly. Example pseudo-code for an DPLL phase computation with shuffled instructions and randomized wait time is shown below in Listing 6.

Listing 6: Pseudo-code for ADPLL phase computation with shuffled instructions and randomized wait time

Note that in this example, the atomic operations for generating y7 and y11 are not data-dependent and thus their order in the pseudo-code can be changed from one iteration of the software loop to another. In this example, the ‘wait r0’ wait instruction is operative to wait one cycle (to simplify the example). In this case, the two shuffled instructions have varied repeating cycles of 19 and 14.

An example listing of a generalized software loop with one or more shuffled instructions is shown in FIG. 41. In this generalized loop, any number of non-data dependent instructions may be randomly shuffled from iteration to iteration. The wait instruction at the end of the loop may be left out depending on the application. In addition, this instruction shuffling embodiment may be used in combination with the previous embodiment of placing a plurality of wait cycle instructions throughout the software loop.

A flow diagram illustrating a second software dithering method of the present invention is shown in FIG. 42. First, the task (e.g., DPLL computation) is partitioned into a plurality of atomic operations (step 440). One or more non-data dependent instructions are shuffled thereby changing the repeating cycles of each instruction (step 442). A random wait pattern is generated for the wait instruction (step 444). The atomic operations of the software loop are executed over a reference clock cycle (step 446). The execution of the wait instruction causes the loop to pause a randomized number of cycles (step 448). The wait period of the wait cycle over each iteration may be set in accordance with a predetermined wait pattern.

A diagram illustrating the current waveform with a different power level for each instruction is shown in FIG. 43. Note that this current waveform corresponds to a fixed software loop instruction pattern.

A diagram illustrating the power spectral density for a software loop with different instruction power is shown in FIG. 44. The power spectral density shown corresponds to the instruction current waveform of FIG. 43 representing a fixed instruction pattern. To make the comparison fair, the average power for each instruction remains the same.

A diagram illustrating the instruction current waveform for a software loop with one or more shuffled instructions is shown in FIG. 45.

Compared to the instruction power graphs of FIGS. 35, 39 and 43 the instruction current waveform of FIG. 45 exhibits a different power for each instruction. This is due to the effect of shuffling the one or more instructions within the software loop from iteration to iteration. The higher the number of unique shuffled instruction loops, the higher the randomization in the instruction current waveform and resultant power spectral density.

A diagram illustrating the power spectral density for a software loop with one or more shuffled instructions is shown in FIG. 46. This figure demonstrates that when shuffling instructions within the loop, the power spectral density changes. Compared to the power spectral density plots of FIG. 44, the main spurs are not significantly different. The spurs surrounding the main spurs, however, are reduced due to the dithering achieved by the instruction shuffling. For example, it can be seen that instruction shuffling achieves a reduction in the spikes of the loop frequency spurs of approximately 1.5 dB/Hz.

Thus, the present invention provides several mechanisms for breaking the software loop pattern to improve the frequency spur performance. These mechanisms include: (1) waiting a random number of cycles at the end of the software, (2) spreading (either randomly or otherwise) a plurality of random wait cycles throughout the software loop thus blending with the loop instructions, and (3) shuffling one or more instructions within the software loop. It is noted that these mechanism may be implemented alone or in any combination in accordance with the particular application and degree of spur reduction desired.

It is important to note that these spurious reductions mechanisms can be made adaptive using close loop control. In this case, the processor monitors the spurious performance by collecting real time or near real time internal DPLL data, e.g., phase error, etc., and analyzes the data to determine the performance. In response, one or more parameters and/or methods are adjusted accordingly to improve the performance until optimum performance is obtained.

Hardware Dithering to Reduce Frequency Spurs

In accordance with the invention, the software dithering method described supra can be applied to a hardware counterpart through the use of clock gating. A block diagram illustrating hardware dithering through clock gating is shown in FIG. 47. The system, generally referenced 450, comprises reconfigurable calculation unit (RCU) 456, a control state machine 454 and clock gating circuit 452.

In this embodiment, the data processing algorithm for the software based DPLL is implemented using hardware that is controlled by the state machine. The control state machine 454 configures the reconfigurable computation unit (RCU) 456 to apply different processing to a particular data sample received on the DATA IN line to generate output data on the DATA OUT line. The state machine waits if it is able to complete the processing required for a data sample before the next data sample arrives. Random waiting cycles can be inserted either through clock gating (driven off the primary clock input) or through the control state machine 454. In this fashion, the three dithering based mechanisms described supra, i.e. (1) waiting a random number of cycles at the end of the software, (2) spreading (either randomly or otherwise) a plurality of random wait cycles throughout the software loop thus blending with the loop instructions, and (3) shuffling one or more instructions within the software loop, are implemented. The first two mechanisms may be implemented either by clock gating or via the control state machine. The third mechanism (i.e. shuffling), is implemented via the control state machine.

The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof.

The corresponding structures, materials, acts, and equivalents of all means or step plus function elements in the claims below are intended to include any structure, material, or act for performing the function in combination with other claimed elements as specifically claimed. The description of the present invention has been presented for purposes of illustration and description, but is not intended to be exhaustive or limited to the invention in the form disclosed. As numerous modifications and changes will readily occur to those skilled in the art, it is intended that the invention not be limited to the limited number of embodiments described herein. Accordingly, it will be appreciated that all suitable variations, modifications and equivalents may be resorted to, falling within the spirit and scope of the present invention. The embodiments were chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated. 

1. A method of reducing the generation of frequency spurs in the performance of a processing task normally performed within a reference clock period, said method comprising the steps of: dividing said task into a plurality of atomic operation computations for execution in a software loop; randomizing the execution of one or more atomic operations in each iteration of said software loop; and wherein said atomic operations are clocked using a processor clock having a frequency significantly higher than that of said reference clock.
 2. The method according to claim 1, wherein said computations of atomic operations are spread out in time throughout said reference clock period to reduce the effects of said frequency spurs.
 3. The method according to claim 1, wherein said processing task comprises a digital phase locked loop.
 4. The method according to claim 1, wherein said step of randomizing comprises the step of dithering the duration of each iteration of said software loop.
 5. The method according to claim 1, wherein said step of randomizing comprises the step of inserting a plurality of random wait cycles throughout said software loop.
 6. The method according to claim 1, wherein said step of randomizing comprises the step of shuffling the order of execution of one or more instructions within said software loop.
 7. The method according to claim 1, further comprising the step of applying closed loop control whereby said step of randomizing is adjusted in accordance with one or more performance data collected from the execution of said processing task.
 8. A method of reducing the generation of frequency spurs in a software based digital phase locked loop normally performed within a reference clock period, said method comprising the steps of: dividing computation of said phase locked loop operation into a plurality of atomic operation computations for execution in a software loop; dithering the duration of each iteration of said software loop; and wherein said atomic operations are clocked using a processor clock having a frequency significantly higher than that of said reference clock.
 9. The method according to claim 8, wherein the average period of execution of said software loop equal to said reference clock period.
 10. The method according to claim 8, said step of dithering changes the spectrum of spurs generated by said atomic computations.
 11. The method according to claim 8, wherein said step of dithering comprises the step of inserting a random wait period at the end of said software loop.
 12. The method according to claim 11, wherein the duration of the random wait period in each iteration of said software loop is set in accordance with a predetermined wait pattern.
 13. The method according to claim 8, wherein all computations required to perform said phase locked loop operation are completed within said reference clock period.
 14. The method according to claim 8, wherein dithering the duration of each iteration of said software loop significantly reduces effects of current transients.
 15. The method according to claim 8, further comprising the step of applying closed loop control to said method whereby said step of dithering is adjusted in accordance with one or more performance data collected from the execution of said digital phase locked loop.
 16. A method of reducing the generation of frequency spurs in a software based digital phase locked loop normally performed within a reference clock period, said method comprising the steps of: dividing computation of said phase locked loop operation into a plurality of atomic operation computations for execution in a software loop; dithering the duration of each iteration of said software loop by inserting a plurality of random wait periods throughout said software loop; and wherein said atomic operations are clocked using a processor clock having a frequency significantly higher than that of said reference clock.
 17. The method according to claim 16, wherein the average period of execution of said software loop is equal to said reference clock period.
 18. The method according to claim 16, said step of dithering changes the spectrum of spurs generated by said atomic computations.
 19. The method according to claim 16, wherein the duration of each random wait period is set in accordance with a predetermined respective wait pattern.
 20. The method according to claim 16, wherein all computations required to perform said phase locked loop operation are completed within said reference clock period.
 21. The method according to claim 16, wherein dithering the duration of each iteration of said software loop significantly reduces the loop frequency spurs.
 22. The method according to claim 16, further comprising the step of applying closed loop control to said method whereby said step of dithering is adjusted in accordance with one or more performance data collected from the execution of said digital phase locked loop.
 23. A method of reducing the generation of frequency spurs in a software based digital phase locked loop normally performed within a reference clock period, said method comprising the steps of: dividing computation of said phase locked loop operation into a plurality of atomic operation computations for execution in a software loop; randomly shuffling the order of execution of one or more atomic operations in each iteration of said software loop; and wherein said atomic operations are clocked using a processor clock having a frequency significantly higher than that of said reference clock.
 24. The method according to claim 23, wherein said one or more shuffled atomic operations comprise non-data dependent atomic operations.
 25. The method according to claim 23, further comprising the step of concatenating a plurality of reshuffled software loops to generate a modified software loop, wherein the atomic operation order of execution in each reshuffled software loop is unique.
 26. The method according to claim 25, wherein higher numbers of concatenated software loops yields higher reductions in loop frequency spurs.
 27. The method according to claim 23, wherein all computations required to perform said phase locked loop operation are completed within said reference clock period.
 28. The method according to claim 23, wherein dithering the duration of each iteration of said software loop significantly reduces loop frequency spurs.
 29. The method according to claim 23, further comprising the step of applying closed loop control whereby said step of randomly shuffling is adjusted in accordance with one or more performance data collected from the execution of said digital phase locked loop.
 30. A phase locked loop (PLL) having a reference clock, said PLL comprising: means for partitioning computation of said phase locked loop into a plurality of atomic operation computations for execution in a software loop; means for randomizing the execution of one or more atomic operations in each iteration of said software loop; a processor clock having a frequency significantly higher than that of said reference clock; an oscillator operative to generate a radio frequency (RF) signal having a frequency determined in accordance with a tuning command input thereto; and a processor operative to generate said tuning command, said processor clocked at said processor clock rate, said processor comprising a calculation unit operative to execute instructions, wherein each instruction is operative to perform one of said atomic operation computations.
 31. The phase locked loop according to claim 30, wherein said means for randomizing comprises the step of dithering the duration of each iteration of said software loop.
 32. The phase locked loop according to claim 30, wherein said means for randomizing comprises the step of inserting a plurality of random wait cycles throughout said software loop.
 33. The phase locked loop according to claim 30, wherein said means for randomizing comprises the step of shuffling the order of execution of one or more instructions within said software loop.
 34. The phase locked loop according to claim 30, further comprising a time to digital converter (TDC) for measuring a phase error between said reference clock and said RF signal.
 35. The phase locked loop according to claim 30, further comprising a clock divider coupled to said oscillator for generation of said processor clock.
 36. The method according to claim 30, further comprising a closed loop control unit whereby said means for randomizing is adjusted in accordance with one or more performance data collected from the execution of said phase locked loop. 